Dynamic control of a homogeneous charge compression ignition engine

ABSTRACT

A homogenous charge compression ignition engine is operated by compressing a charge mixture of air, exhaust and fuel in a combustion chamber to an autoignition condition of the fuel. The engine may facilitate a transition from a first combination of speed and load to a second combination of speed and load by changing the charge mixture and compression ratio. This may be accomplished in a consecutive engine cycle by adjusting both a fuel injector control signal and a variable valve control signal away from a nominal variable valve control signal. Thereafter in one or more subsequent engine cycles, more sluggish adjustments are made to at least one of a geometric compression ratio control signal and an exhaust gas recirculation control signal to allow the variable valve control signal to be readjusted back toward its nominal variable valve control signal setting. By readjusting the variable valve control signal back toward its nominal setting, the engine will be ready for another transition to a new combination of engine speed and load.

This invention was made with Government support under DOE Contract No. DE-FC26-05NT4 2412 awarded by the U.S. Department of Energy. The Government has certain rights to this invention.

TECHNICAL FIELD

This disclosure relates generally to homogeneous charge compression ignition (HCCI) engines, and more particularly to transitioning from a first combination of speed and load to a second combination of speed and load.

BACKGROUND

A relatively new combustion strategy known as homogeneous charge compression ignition (HCCI) shows great promise in reducing undesirable emissions from internal combustion engines that utilize a compression ignition strategy. HCCI refers generally to the idea of mixing fuel with air in the engine cylinder before autoignition conditions arise. The mixture is compressed to autoignition, with a general desirability that the combustion event take place in the vicinity of top dead center. Although HCCI has proven the ability to drastically reduce undesirable emissions, especially NOx, the combustion strategy has brought new problems that must be overcome in order to render such an engine commercially viable. For instance, for an HCCI engine to be a viable alternative to a counterpart conventional diesel engine, it must have the ability to operate effectively over a relatively wide load range. One problem encountered with HCCI engines is the extreme sensitivity and difficulty in controlling ignition timing. In addition, HCCI engines can have difficulty in operating in higher load ranges where more fuel is supplied to the individual cylinders. This perceived limitation may be due to extreme pressure spikes that occur when the charge burns. The pressures can rise so fast and get so high as to exceed the vibrational and structural containment capability of an engine housing. Thus, operating an HCCI engine, especially at higher speeds and loads, can be extremely problematic, but must be overcome to enable such an engine to be a viable alternative to a counterpart conventional diesel engine.

Apart from problems associated with high load operation, multi-cylinder HCCI engines have even more problems that need to be overcome. For instance, engine geometry, including the intake geometry, fuel injector performance variations, and other known and unknown influences affect the specific burn behavior of charges in different ones of a plurality of engine cylinders. For instance, intake manifold geometry may result in one cylinder receiving less or more air than other cylinders, and a fuel injector performance variation in another cylinder may cause less or more fuel to be injected based upon the same control signal. These differences result in different air/fuel ratios in different cylinders. HCCI combustion is very sensitive to air/fuel ratio and other factors including charge mass, compression ratio, as well as the initial temperature and pressure of the charge when compression begins. Thus, these variations can contribute to substantial differences in both heat release and combustion phase timing among a plurality of different engine cylinders. While some variation may be acceptable at lower load conditions, at higher speeds and loads, combustion phasing and heat release variations among the plurality of cylinders can give rise to unacceptable noise levels. In addition, assuming equal air/fuel ratios, the cylinder with the most advanced combustion timing will develop a maximum pressure and pressure rise rate at a lower load, and therefore will limit peak load of the entire engine. Those skilled in the art will appreciate that, when the charge burns too early in the combustion stroke, excessive cylinder pressures and pressure rise rates can occur that limit the load carrying capability of that cylinder, and hence the entire engine.

In addition to the above problems associated with ignition timing, controlling peak pressures and pressure rise rates, and balancing combustion among a plurality of engine cylinders, there are even more problems when there is recognition that the engine must not only have the capability of operating in a steady state condition, but also must have the capability of transitioning among different combinations of speed and load. This problem is further compounded by recognition that different control strategies are so cross-coupled in their influence on engine behavior that no known control strategy is available for an HCCI engine that allows the engine to retain stable operation across a wide range of engine speeds and loads. In addition, some potential control techniques, such as varying exhaust gas recirculation rates and/or varying geometric compression ratio in the engine, may be too sluggish to react on an engine cycle to cycle basis. As used in this text, the term “geometric compression ratio” means the ratio of the cylinder volume when the engine piston is at bottom dead center to the volume of the cylinder when the piston is at top dead center. If the engine is too sluggish in transitioning from one combination of speed and load to another combination of speed and load, that behavior could also render it not viable as an alternative to a convention diesel engine.

Other potential control actuators may include fuel injection timing and quantity control, as well as variable intake and/or exhaust valve timing control. While these types of control actuators may have the ability to adjust from one engine cycle to the next engine cycle, a variable valve actuator alone may not provide a sufficient bandwidth of control to enable the engine to operate across a wide range of speeds and loads. For instance, a variable valve actuator, such as a variable intake valve actuator may not have a bandwidth that permits the engine to operate beyond a narrow range of speeds and loads without some other additional strategy. In addition, adjustments to variable intake valve actuators not only changes the compression ratio, but also the charge mass and the initial cylinder charge pressure and temperature. These factors interact to determine when auto-ignition conditions arise, if at all, in the engine cylinder.

In addition, further problems can occur by recognizing that control actuators may not actually be doing what the engine controller expects. For instance, if exhaust gas recirculation is controlled, even slight differences between the expected exhaust gas recirculation rate and the expected or desired rate can result in substantial variations in engine behavior. Thus, some of the control actuators themselves may need their own separate feedback control in order to be realistically utilized in the highly combustion-sensitive environment of a homogeneous charged compression ignition engine. Thus, the limited bandwidths of available control actuators, their interactions in altering combustion behavior, and uncertainties in the control actuators doing what the engine controller expects renders the problems associated with dynamic control of an HCCI engine nearly insurmountable.

One strategy for dealing with the problems of HCCI is described in co-owned U.S. Pat. No. 6,725,838. This reference describes a mixed mode strategy where HCCI is employed over a lower load range portion of the engine, and conventional diesel engine strategies are employed at high speeds and loads. By conventional, this disclosure means that fuel is injected directly into an engine cylinder after autoignition conditions have arisen, with the injection taking place in the vicinity of top dead center. While a mixed mode strategy can produce superior emissions compared to that of a conventional diesel engine, it requires increased complexity, especially in manufacturing and controlling the fuel system, but mixed mode still results in more undesirable emissions than that possible with an entirely HCCI operation strategy.

The present disclosure is directed toward one or more of the problems set forth above.

SUMMARY OF THE DISCLOSURE

In one aspect, a method of operating an engine includes compressing a charge mixture of air, exhaust and fuel in a combustion chamber to an auto ignition condition of the fuel. The engine is transitioned from a first combination of engine speed and load to a second combination of speed and load by changing the charge mixture. The changing step includes adjusting, for a consecutive engine cycle, both a fuel injector control signal and a variable valve control signal away from a nominal variable valve control signal. The changing step also includes readjusting the variable valve control signal back toward the nominal variable valve control signal by adjusting at least one of a geometric compression ratio control signal and an exhaust gas recirculation control signal over a plurality of engine cycles following the consecutive engine cycle.

In another aspect, an engine includes a fuel injector positioned for direct injection of fuel into each of at least one combustion chamber. At least one gas exchange valve is associated with each combustion chamber. A variable valve actuator is operably coupled to a gas exchange valve of each combustion chamber. The engine also includes an exhaust gas recirculation control valve and a variable geometric compression ratio device for varying a geometric compression ratio of each combustion chamber. An electronic controller is in control communication with the fuel injector, the variable valve actuator, the exhaust gas recirculation control valve and the variable geometric compression ratio device. The electronic controller is configured to compress a charge mixture of fuel, air and exhaust to an auto ignition of the fuel. The electronic controller is configured to transition from a first combination of speed and load to a second combination of speed and load by changing the charge mixture. The electronic controller is also configured to change the charge mixture for a consecutive engine cycle by adjusting both the fuel injector control signal and a variable valve control signal away from a nominal variable valve control signal. The electronic controller is also configured to readjust the variable valve control signal back toward the nominal variable valve control signal by adjusting at least one of a geometric compression ratio control signal and an exhaust gas recirculation control signal and an exhaust gas recirculation control signal over a plurality of engine cycles following the consecutive engine cycle.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a schematic illustration of a homogeneous charge compression ignition engine according to one aspect of the present disclosure;

FIG. 2 is a second embodiment of an engine schematic according to the present disclosure;

FIG. 3 is a schematic view of an individual combustion chamber for the engine of FIGS. 1 and 2;

FIGS. 4 a-4 d are graphs of heat release verses engine crank angle for the engine of FIG. 1 or 2 before any trimming, with fuel trims, with intake valve trims and with both fuel and intake valve trims, respectively;

FIG. 5 is a graph of charge mass percentage of air, exhaust and fuel, respectively, verses load according to one aspect of the present disclosure; and

FIG. 6 is a graph of compression ratio verses load showing an available control bandwidth for both a geometric compression ratio controller and a variable valve compression ratio controller.

DETAILED DESCRIPTION

Referring to FIG. 1, a homogeneous charge compression ignition engine 10 includes an engine housing 12 that includes a plurality of cylinders or combustion chambers 14 disposed therein. In the illustrated embodiment, engine 10 includes six cylinders 14, but those skilled in the art will appreciate that engine 10 could include any number of cylinders without departing from the present disclosure. Engine 10 includes a conventional radiator 13 along with a cooling system (not shown) to cool the engine in a conventional manner. Each cylinder 14 preferably includes a fuel injector 16 positioned for direct injection of liquid fuel into the individual cylinders. Furthermore, each fuel injector may include a nozzle tip configured to produce a shower head spray pattern 25 in which fuel injection plumes point at a plurality of different angles with respect to a fuel injector centerline. Furthermore, the fuel injection holes may be constructed using known laser drilling techniques to achieve extremely small diameter openings, which may be on the order of 80-100 microns. Those skilled in the art will appreciate that the small holed shower head spray pattern can facilitate better fuel and air mixing, and possibly permit lower injection pressures without wetting the walls of cylinder 14, which could produce undesirable unburnt hydrocarbon emissions and/or particulate matter.

Engine 10 may also be equipped with a variable geometric compression ratio control device 80 that allows for the compression ratio of all cylinders 14 to be adjusted simultaneously. Although the variable geometric compression ratio control device 80 could take on a variety of forms, it may have a structure similar to that described in co-owned published United States Patent Application 2006/0112911. In that disclosure, an eccentric crank variable compression ratio mechanism raises and/or lowers the crankshaft in the engine housing to alter the compression ratio of all of the cylinders uniformly. Nevertheless, those skilled in the art will appreciate that any appropriate strategy for varying compression ratio may be considered appropriate for an engine 10 according to the present disclosure. Those skilled in the art will appreciate that having the ability to vary compression ratio can render the problem of combustion control timing and the problem associated with extremely high pressures during combustion more manageable than with a fixed compression ratio engine. Nevertheless, fixed geometric compression ratio engines are still within the intended scope of the disclosure.

Engine 10 may also be constructed to include variable intake valve actuators 81 as an alternative, or in addition to, the variable geometric compression ratio device 80. Those skilled in the art will appreciate that the variable intake valve actuator can also take on a variety of forms, such as purely electronically controlled, or a hybrid that uses cam actuation and a special hydraulic actuator to hold the intake valve open beyond a cam dictated valve closing timing. The later alternative is described, for instance, in co-owned published U.S. Patent Application 2003/0116124. This variable timing capability can also be exploited to adjust compression ratio in the individual cylinders by adjusting the timing at which the intake valve closes. In addition, variable valve timing affects combustion phasing by adjusting the charge mass in the cylinder, apart from compression ratio. Engine 10 may also be equipped with variable exhaust valves (not shown) as an alternative, or in addition to the variable intake valve actuators 81. Unlike the variable geometric compression ratio device 80, each individual cylinder includes an individually controllable variable intake valve actuator 81, which allows the behavior of each cylinder 14 to be individually controlled. Preferably, engine 10 is equipped with both a variable geometric compression ratio device 80 and variable intake valve actuators 81 that allow en banc adjustments of all cylinders 14 via the variable geometric compression ratio device 80, and then finer and faster control of combustion phasing in individual cylinders 14 via the variable intake valve actuators 81.

Engine 10 may also be equipped with some means for detecting the timing of combustion events in each individual cylinder 14 so that that information can be fed back to a combustion controller, which may then use that information to adjust combustion timing for a subsequent event. In the illustrated embodiment, an individual combustion pressure sensor or an ion sensor 84 is associated with each of the individual cylinders 14. Nevertheless, those skilled in the art will appreciate that any single or multiple sensor strategy that permits the timing of combustion events in each of the cylinders 14 to be determined in real time would be suitable for engine 10 of the present disclosure, and may be desirable to better enable closed loop combustion timing control.

Engine 10 also includes a fresh air inlet 17, a tail pipe 18 and an exhaust gas recirculation system 20. A combination of fresh air and exhaust gas are supplied to engine intake manifold 73 via an engine intake passage 72, which is separated from an air/exhaust gas passage 70 by an air-to-air after cooler 71. Those skilled in the art will appreciate that cooler 71 may include measures, such as being made at least partially from stainless steel, to resist the corrosive influences of exhaust gas passing therethrough. In addition, cooler 71 may include any suitable heat exchanger, including liquid to gas, etc. Exhaust from the individual cylinders 14 collect in first and second exhaust manifolds 50 a and 50 b, which are respectively connected to exhaust passages 51 a and 51 b. Nevertheless, those skilled in the art will appreciate that a single exhaust manifold and exhaust passage could be utilized without departing from the scope of the present disclosure. The exhaust passages 51 a and 51 b feed into a turbine 52 of a turbocharger 22 in a conventional manner. However, a portion of the exhaust that would otherwise go to turbine 52 is instead routed into branch recirculation passages 60 a and 60 b, which merge in the vicinity of a coated diesel particulate filter 61. Those skilled in the art will appreciate that particulate filter 61 may be coated with any suitable catalyst for any desired purpose, such as to clean the high pressure exhaust being recirculated via these passages. In addition, those skilled in the art will appreciate that particulate filter 61 is preferably positioned in close enough proximity to cylinders 14 that it can be regenerated via heat supplied by the engine. Alternatively, a separate auxiliary regeneration device, which produces its own heat, may be positioned in close proximity to particulate filter 61 to facilitate its regeneration. After passing through particulate filter 61, the high pressure exhaust passes through a clean gas intake cooler 62 and a control valve 28 before connecting to the throat of a venturi 64, which empties into air/exhaust gas return passage 70. Control valve 28 may take on a variety of forms, but may be a relatively simple two-position valve that is never fully closed. For instance, the flow area through control valve 28 in its first position may be chosen to facilitate a desired exhaust gas recirculation level associated with low load or idle conditions, and a second or more fully open position may be associated with higher speeds and loads to facilitate higher volumes of exhaust gas recirculation. Nevertheless, control valve 28 may have more than two positions, and may even include a fully closed position, if desired. Control valve 28 is controlled by an electronic control module 29 via a communication line 30 in a conventional manner.

Medium pressure exhaust gas leaves an axial passage from turbine 52 into an inter turbine passage 53, which connects to a turbine 54 of a second turbocharger 23 which is in series with turbocharger 22. Turbine 54 may be an axial turbine, and its lower pressure axial outlet empties into turbine outlet 55. Before arriving at tail pipe 18, the relatively low pressure exhaust is passed through a coated diesel particulate filter 57, which may include any suitable catalyst to treat the exhaust prior to exiting tail pipe 18. Because particulate filter 57 may be relatively remote from the heat of the individual cylinders 14, an auxiliary regeneration device 56 may be included in order to provide the heat necessary to regenerate particulate filter 57. After exiting particulate filter 57, a portion, which may be all of the exhaust gas, exits at tail pipe 18. However, a portion of that low pressure exhaust may be recirculated via low pressure exhaust passage 35. The low pressure exhaust gas is cooled in a clean gas intake cooler 40 prior to encountering a control valve 26. Control valve 26 may have a plurality of discrete positions, or may have a complete continuum of positions from a fully closed to a fully opened position, depending upon the desired action and sophistication of the exhaust gas recirculation system 20. Control valve 26 may be controlled by electronic control module 29 via communication line 32.

Fresh air entering fresh air inlet 17 passes through a throttle control valve 27 prior to entry into a fresh air supply passage 19, which merges with low pressure exhaust passage 35 at a tee connection 42. Throttle control valve 27 is controlled in its positioning by electronic control module 29 via a communication line 31. Those skilled in the art will appreciate that throttle control valve 27 may have a continuum of positions ranging from a restricted fully throttled position that still allows some fresh air to enter the system, to an unrestricted fully open position. The mixture of low pressure exhaust gas and fresh air is supplied to compressor 49 of turbocharger 23 via compressor supply passage 43. Those skilled in the art will appreciate that compressor 49 may include measures, such as use of corrosion resistant titanium, to deal with the corrosive influence, if any, existing in the exhaust gas passing through the compressor. An inter compressor passage 46 connects compressor 49 to compressor 48 of turbocharger 22. An inter cooler 45 may be included in inter compressor passage 46 to cool the compressed exhaust/air mixture. In addition, cooler 45 may include corrosion resistant materials, such as stainless steel, to avoid or reduce the corrosion influences, if any, of the exhaust gas. Like compressor 49, compressor 48 may include corrosive resistant materials such as titanium, to reduce or avoid corrosive influences from the exhaust gas. A air/exhaust mixture passage 47 fluidly connects the outlet of compressor 48 to the inlet of venturi 64. Thus, venturi 64 represents the mixing location for exhaust from the high pressure side of the exhaust gas recirculation system 20 with low pressure exhaust that originated near the tail pipe, but has had its pressure boosted as a result of passing through compressors 48 and 49.

If desired, coolers 45 and 71 may be connected to a condensate pump 76 via respective condensate passages 78 and 77, to facilitate removal of collected condensed water and other liquids in coolers 45 and 71 in a conventional manner. Although not necessary, engine 10 may also include one or more NOx/lambda sensors 85 and 87 at specific locations in order to allow for gas constituent levels to be monitored during operation of engine 10. In particular, the lambda sensors 85 and 87 may monitor the contents of several different gases in air/exhaust gas return passage 70, and this information may be used to further facilitate combustion control of combustion events in the individual cylinders 14.

Although engine 10 is illustrated as including staged turbochargers 22 and 23, those skilled in the art will appreciate that the engine could include a single turbocharger without departing from the scope of the present disclosure. In such a case, the high pressure exhaust return could connect upstream from the turbocharger, whereas the low pressure exhaust gas return would connect downstream from the same. Those skilled in the art will appreciate that the relative proportions of exhaust gas to fresh air are controlled by electronic control module 29 by appropriately positioning control valves 26, 27 and 28. When the relatively high proportions of EGR are demanded, such as on the order of 50% or more, electronic control module 29 throttles control valve 27 to restrict the supply of fresh air, and moves valves 26 and 28 towards there fully opened positions to enable the higher ratios of exhaust gas recirculation associated with desired operating conditions at higher speeds and loads for engine 10.

Referring now to FIG. 2, a homogeneous charge compression ignition engine 110 is shown with many features that are identical to engine 10 described earlier. However, the exhaust gas recirculation system 120 includes several differences relative to the exhaust gas recirculation system 20 described in relation to engine 10. In particular, while exhaust gas recirculation system 120 includes a pair of staged turbochargers 122 and 123 in series, there is only a single medium pressure exhaust gas recirculation passage 163 rather than the separate high and low pressure exhaust gas return passages associated with engine 10. In exhaust gas recirculation passage 120, the exhaust gas is supplied to turbine 152 of turbocharger 122 and the medium pressure exhaust gas exits turbine 152 via an axial passage connected to medium pressure exhaust gas recirculation passage 163, and via a separate inter turbine passage 153 that connects to turbine 154 of turbocharger 123. The low pressure exhaust then exits turbine 154, which may be an axial turbine, and empties into turbine outlet 155 before passing through a coated diesel particulate filter 157. As in the previous embodiment, the particulate filter 157 may include any suitable catalyst coating and may include any auxiliary regeneration device 156 that generates the heat necessary to regenerate particulate filter 157. After traversing particulate filter 157, the exhaust gas passes a NOx/lambda sensor 187 on its way out of the tail pipe 18.

The medium pressure exhaust exiting turbine 152 into medium pressure exhaust recirculation passage 163 passes through a coated diesel particulate filter 161 and then enters a clean gas intake inter cooler 162. Meanwhile, fresh air enters at fresh air intake 17 and passes through a throttle control valve 27 into a fresh air supply passage 19. The fresh air is then compressed in compressor 149 of turbocharger 123 before entering air supply passage 143, which merges with medium pressure exhaust gas recirculation passage 163 in cooler 162. Cooler 162 empties into an inter compressor passage 146 that connects to compressor 148 of turbocharger 122. Compressor 148 may include corrosion resistant materials, such as titanium, to better resist a corrosive influence, if any, from the exhaust gas being recirculated. The compressed mixture of exhaust gas and fresh air leaves turbocharger 148 and enters exhaust gas recirculation passage 170, where it passes a lambda sensor 185 on its way to the engine intake passage via an air to air after cooler similar to that described with regard to the previous embodiment. As in the previous embodiment, throttle control valve 27 is controlled via electronic control module 129 via a communication line 131. Thus, the exhaust gas recirculation system 120 of the embodiment of FIG. 2 is simplified over that of the embodiment of FIG. 1 in that the ratios of exhaust gas to fresh air is controlled entirely by appropriately positioning throttle control valve 27, rather than by utilizing three valves as in the previous embodiment.

Those skilled in the art will appreciate that HCCI operation is very sensitive to air/fuel ratio, charge mass, initial cylinder conditions (P and T at valve closing) and compression ratio. As a consequence, a slight difference in any one of the air/fuel ratio, charge mass or compression ratio between two different cylinders can result in substantial differences in both combustion phase timing and combustion heat release. Small variations in air fuel ratio and/or charge mass can have a variety of sources. For instance, geometry of the air intake manifold as well as the position of the individual cylinder with respect to that manifold can affect small differences among different cylinders in the amount of air (and exhaust from EGR) that reaches that individual cylinder. In addition, less than thoroughly mixed exhaust gas with fresh air can also alter conditions in a specific cylinder. Another possible source of variation in air/fuel ratio and/or charge mass can be attributed to performance variations among different fuel injectors. For instance, the same control signal delivered to a plurality of different fuel injectors will inherently result in slightly different amounts of fuel being injected by the different fuel injectors. Better or worse spray atomization may also contribute to variations in individual cylinder performance. In any event, without any adjustments among the plurality of engine cylinders 14, there will be variations in combustion phase timing and combustion heat release. Although not readily apparent, the cylinder with the most advanced combustion phase timing can limit the overall load range of the entire engine. As load increases, this early firing cylinder will eventually cause pressure rise rates and pressure maximum limits in that individual cylinder to be exceeded before that of the others. In addition, variations in combustion phase timing and combustion heat release can also lead to ever increasing amounts of noise as engine load increases. Thus, those skilled in the art will recognize that inherent variations among different engine cylinders 14 will otherwise limit the load range of the entire engine unless some measure is taken to balance or reduce variations in combustion phase timing and/or combustion heat release among the engine cylinders.

Referring now to FIGS. 3 and 4 a-d, a typical engine cylinder 14 for the engines 10 and 110 of FIGS. 1 and 2 is illustrated. Cylinder 14 includes a reciprocating piston 15 and an electronically controlled fuel injector 16 positioned for injection of liquid fuel directly into cylinder 14. Fuel injector 16 includes an electrical actuator 21 operable to control fuel injection quantity from fuel injector 16 via control signals transmitted from engine controller 29 via communication line 33. The engine controller is configured to make independent adjustments in fuel injection quantity to individual cylinders 14 via different control signals communicated to different fuel injectors 16 associated with the different cylinders 14. As used in the present disclosure, fuel injectors 16 can be thought of as combustion heat release controllers. In other words, by adjusting individual signals to individual fuel injectors 16, the fuel injectors can be adjusted in their fuel injection quantity to result in less variation in combustion heat release among all of the engine cylinders 14. For instance, a cylinder with a higher than average combustion heat release may have its variation reduced by altering its control signal to slightly reduce the quantity of fuel that the fuel injector 16 for that individual cylinder 14 injects. Those skilled in the art will appreciate that engine controller 29 may be configured to have a closed loop control strategy for continuously adjusting combustion heat release whenever the engine 10, 110 is in operation. Nevertheless, those skilled in the art will appreciate that the present disclosure also contemplates a non-closed loop strategy where the individual control signal adjustments to the various cylinders are preset, and may be updated on some periodic bases, such as at each engine startup or during routine servicing intervals.

In closed loop operation, the engine controller 29 determines a combustion heat release for combustion in the different engine cylinders 14 in one engine cycle, and then determines which of the engine cylinders are in need of having their combustion heat released adjusted to reduce variation. If a cylinder is in need of adjustment, the engine controller 29 will determine a fuel injector control signal adjustment that will either increase or decrease the combustion heat release for that individual cylinder. In the illustrated embodiment, determination of combustion heat release is accomplished by individual combustion sensors 84 associated with each individual cylinder 14 that communicate information to engine controller 29 via communication lines 37. In the illustrated embodiment, combustion sensor 84 is a pressure sensor, but those skilled in the art will appreciate that other sensors such as ion sensors or any suitable strategy known in the art that can be utilized to estimate combustion heat release for an individual cylinder could be utilized. In the present disclosure, each individual cylinder 14 includes its own combustion sensor 84. However, the present disclosure also contemplates strategies where each individual cylinder includes more than one sensor to determine combustion characteristics, or a strategy that includes a number of sensors less than the number of engine cylinders, but still able to determine individual combustion characteristics sufficient to carry out the control strategy of the present disclosure. Depending upon the desired sophistication and possibly the speed of engine controller 29, combustion heat release can be estimated in a number of ways. A general equation for the apparent heat release rate may be expressed as

$\frac{\mathbb{d}Q}{\mathbb{d}t} = {{\frac{r}{r - 1}P\frac{\mathbb{d}V}{\mathbb{d}t}} + {\frac{1}{r - 1}V\frac{\mathbb{d}p}{\mathbb{d}t}}}$ where: Q = heat  release r = ratio  of  specific  heats P = pressure  at  time  tV = instantaneous  combustion  chamber  volume For instance, a simple numerical integration strategy could be utilized on the entire equation over the combustion duration. Alternatively, an adequate estimation of combustion energy release can be obtained with less intensive processing by recognizing that the dv/dt term in the equation may be ignored if HCCI combustion occurs near top dead center. Those skilled in the art recognize that because combustion chamber volume changes very little in the brief time it takes for the charge to burn around TDC. In one insightful alternative, even numerical integration can be avoided by recognizing that the maximum dQ/dt in the above equation correlates directly to the total Q or heat release. Thus, if one cylinder shows a maximum dQ/dt that is high, the control signal to that fuel injector would be shortened to decrease the quantity of fuel in order to decrease the maximum dQ/dt and hence the total heat release. Likewise, if the maximum dQ/dt for an individual cylinder is low, the control signal to the fuel injector for that signal would be lengthened to increase the quantity of fuel, increase the maximum dQ/dt and hence bring the total heat release for that cylinder into balance with the other cylinders. Thus, any level of sophistication can be applied to estimate combustion heat release, provided that strategy allows engine controller 29 to determine variation among the cylinders in combustion heat release with sufficient accuracy to adjust control signals to the individual fuel injectors 16 accordingly. Thus, in closed loop operation, the variation among the individual cylinders in combustion heat release can be decreased to a point that the variation is acceptable. This aspect of the disclosure is illustrated in FIGS. 4 a and 4 b. The combustion heat release variation 92 shown in FIG. 4 a before any control signal adjustments can be compared with the relatively smaller variation 94 shown in FIG. 4 b after the fuel injector control signals for the individual cylinders 16 have been adjusted. Those skilled in the art will appreciate that the fuel injector control signals can be adjusted toward an average of the cylinders or toward some predetermined combustion heat release for that specific operating condition of engine 10, 110.

Apart from reducing variations among the individual cylinders in combustion heat release, engines 10 and 110 may also include a means for individually adjusting combustion phase timing in the individual cylinders 14. Thus, the present disclosure contemplates individual combustion phase controllers associated with each of the individual cylinders 14. In the illustrated embodiment, these combustion phase controllers take the form of variable intake valve actuators 81 that allow for the intake valve 82 to be held open beyond a cam dictated closing timing determined by the lobe position of cam 83. Combustion phase controlling may also be controlled by a variable exhaust valve actuator 88 associated with exhaust valve 86 and cam 89. Although the present disclosure illustrates variable valve timing via valve actuators that work in conjunction with cams 83 and 89, those skilled in the art will appreciate that either the intake and/or exhaust may be totally electronically controlled, such as via hydraulic actuators of the type known in the art. In the illustrated embodiment, the variable intake valve actuators 81 are controlled by engine controller 29 via communication lines 34, and variable exhaust valve actuators 88 are controlled via communication lines 36. Thus, by adjusting individual control signals to one or both of the variable valve actuators 81 and 88, the amount of gas received in that cylinder 14, and the initial pressure, can be adjusted to adjust the charge mass. This in turn adjusts the air/fuel ratio as well as the pressure and temperature at TDC in that individual cylinder 16, and hence the combustion phase timing in that cylinder. In addition, combustion phasing is controlled by actual compression ratio, which is determined by the ratio of cylinder volume when the valve(s) close to the cylinder volume at top dead center.

Combustion phase timing can be based upon any suitable combustion characteristic, such as maximum dp/dt or maximum pressure. The illustrated embodiment identifies combustion phase timing at the inflection point of the pressure versus time trace reflected by maximum dp/dt. Thus, the same combustion sensor 84 may be utilized to determine combustion phase timing for an individual cylinder 14 by determining the timing at which the peak cylinder pressure rise rate occurs. This information can then be utilized, and a comparison between all of the engine cylinders can be performed, and variation among the cylinders can be reduced by adjusting individual variable valve actuators 81 and/or 88 for that cylinder in a subsequent engine cycle. Nevertheless, those skilled in the art will appreciate that a separate different sensor could be utilized for determining combustion phase timing determination apart from the pressure sensor 84 illustrated. In the event that combustion phase timing is adjusted using only the variable intake valve actuator 81, closing the intake valve 82 later in an engine cycle will reduce charge mass and compression ratio, which will retard combustion phase timing. On the other hand, closing the intake valve 82 earlier in the engine cycle will increase charge mass and compression ratio which will advance combustion phase timing. FIGS. 4 a and 4 c are useful in illustrating this concept. In the case of FIG. 4 a, the combustion phase timing variation 91 is relatively large, but after the individual cylinders have been trimmed by adjusting individual control signals to the respective variable intake valve actuators 81, the variance is reduced as shown in FIG. 4 c to a small phase timing variation 93. FIG. 4 d is of interest for showing the combustion heat release traces after both the combustion phase timing and combustion heat release magnitude variations have been reduced.

Depending upon the specific structure and actuators, each engine 10, 110 according to present disclosure can be thought of as including an exhaust gas return rate control system. In the case of engine 10, the exhaust gas return rate control system includes control valves 26, 27 and 28 as well as possibly some known structure and mechanism (not shown) for controlling boost pressure in a known manner. On the other hand the engine 110 may have its exhaust gas return rate control system constituted by control over turbochargers 122 and 123 to control boost pressure in a conventional manner as well as throttle control valve 27. Referring now to FIG. 5, a graph of mass percentage of exhaust gas, air and fuel is illustrated across the load range for engine 10, 110. As can be seen, the mass percentage of exhaust to air is relatively low at a low load range and actually is greater than the mass quantity of air at higher load ranges. In fact, the EGR rate may be in excess of 50% at the highest load operating ranges. Those skilled in the art will appreciate that the available EGR rates are practically limited on the top side by a smoke limit and/or a misfire limit, and on the lower side by a NOx limit and/or peak rise rate limit. Those skilled in the art will appreciate that increasing EGR rates can eventually lead to a point where the combustion event can be starved of air, thereby producing smoke. In addition, even higher EGR rates can actually cause a misfire. Thus, with all other things being equal, increasing an EGR rate will retard combustion timing, and increase the combustion duration, whereas a reduction in EGR will advance ignition timing, and reduce the combustion duration. The misfire limit typically comes more into play at low loads, whereas the smoke limit will typically come more into play at higher loads. Those skilled in the art will also appreciate that the peak rise rate of combustion is substantially affected by the amount of diluent or exhaust gas in the engine cylinder 14. Additional exhaust gas percentage will generally reduce peak combustion pressure, reduce the pressure rise rate and retard combustion phase timing for the combustion event, as well as extending the duration of the combustion event. Decreased exhaust gas percentage will generally increase peak combustion pressure, increase the pressure rise rate, advance combustion phase timing, and shorten the duration of the combustion event. Those skilled in the art will also appreciate that the EGR rate affects the NOx level of the combustion event. Generally, the exhaust gas acts as a heat sink and therefore cooler combustion and hence less NOx will be produced at elevated levels of exhaust gas in the cylinder. Those skilled in the art will thus realize that a variety of different considerations must be taken into account before setting the exhaust gas return rate at each individual operating condition. However, one can expect the exhaust gas rate settings to vary substantially at different speeds and loads in order to achieve overall acceptable operation with the best mixture of undesirable emissions, which includes NOx, particulate matter and hydrocarbons.

Referring now to FIG. 6, although the geometric variable compression ratio control device 80 may have a relatively large bandwidth, the majority of that bandwidth will be taken up over the load range of the engine. This aspect of the disclosure illustrated by the downward sloping diagonal line indicated as a geometric compression ratio setting. At lower loads, it may be desirable to operate at a relatively high geometric compression ratio in order to better avoid misfires and promote better operation of the engine with regard to emissions. On the other hand, at higher loads it may be desirable to operate at the lower end of the geometric compression ratio bandwidth. At high loads, the problems associated with controlling combustion ignition timing, pressure rise rates, peak cylinder pressure all become simultaneously more problematic. However, lower compression ratios at higher loads can serve to make all of these problems more manageable. Depending upon the specific engine geometry, the desired geometric compression ratio at low loads may be as much as double or more than the desired geometric compression ratio at the highest load range for the engine. Thus, the compression ratio control system for the HCCI engine must have a substantial range of capabilities in order to allow the engine to operate across a wide load range. Those skilled in the art will appreciate that virtually all aspects of the operation of a homogenous charge compression ignition engine become more acute at higher loads.

FIG. 6 is also of interest for showing that the variable intake valve actuator (IVA) permits a bandwidth of control about the geometric compression ratio setting. Thus, the variable intake valve actuator 81 can be relied upon for quick changes in compression ratio from cycle to cycle and also to trim variations among individual cylinders as discussed above. Thus, in the short term when load changes, the compression ratio target will be primarily changed quickly by adjustments to the variable intake valve actuators 81, but in the longer term the compression ratio target may preferably be met by adjusting the geometric compression ratio via device 80 as discussed above. Those skilled in the art will appreciate that, depending upon the specific structure and control features of an HCCI engine, other short term and long term strategies could be utilized to satisfy the compression ratio target as illustrated in FIG. 6. For instance, another HCCI engine might be equipped with variable geometric compression ratio controllers individually associated with each of the individual cylinders, and those actuators may have a quick enough response time to take the place of the en banc geometric compression controller 80 and variable intake valve actuators 81 or the engines 10, 110 illustrated in FIGS. 1 and 2. In other words, the same compression ratio control features may be used for both trimming combustion phase timing among the individual cylinders, and also for controlling the engine to arrive at a combustion ratio target at each different speed and load across the engine's operating range. These other strategies are within the contemplated scope of the present disclosure.

Because of the great complexities in operating an HCCI engine, especially at higher loads, it may be desirable to predetermine geometric compression ratio and exhaust gas return rates at each speed and load. These predetermined settings would each correspond to an acceptable mixture of performance, emissions and other concerns at each speed and load across the engine's operating range. These settings may be saved as respective geometric compression ratio controller settings and exhaust gas return rate controller settings that are mapped as a function of speed and load, and available on a medium linked to the electronic engine controller 29. Even with these premapped settings, it may be desirable to have closed loop control on at least one of the exhaust gas return controller system and the geometric compression ratio controller system. For instance, the lambda sensor 85, which is positioned downstream from the exhaust gas return rate controller system, allows for the engine controller 29 to confirm the exhaust gas ratio actually being supplied to the engine corresponds to what engine controller 29 believes that rate is or should be. This affords the ability to adjust the controller settings in order to achieve a return rate at a desired level, rather than operating in an open loop fashion. Likewise, the geometric compression ratio sensor 79 allows for the engine to confirm, and possibly adjust signals to, the geometric compression ratio control system 80 to make the engine configuration better correspond to the predetermined maps and/or the expected compression ratio.

To summarize, steady state operation at a given speed and load may be accomplished by setting the geometric compression ratio control device according to a look up table of speed and load, setting the exhaust gas recirculation rate according to another look up table based upon speed and load, balancing heat release among the combustion chambers via feedback control of fuel injector signals, and adjusting combustion phase timing via individual adjustments to variable valve actuators associated with each of the combustion chambers. In addition, depending upon the sophistication of the control strategy, the exhaust gas recirculation system and the geometric compression ratio device may have feedback sensors so that the controller can confirm that the exhaust gas recirculation rate and geometric compression ratio are actually where the controller expects them to be. Thus, the controller may be equipped with maps of geometric compression ratio, exhaust gas recirculation rate, desired combustion phasing and desired heat release rate for each speed and load across the engines operating range. Even when operating at a steady state condition, all four control devices may be having their control signals continuously adjusted to maintain a charge mixture and compression ratio, and hence steady state combustion. However, in order to be viable as an alternative to a conventional diesel engine, the HCCI engine must also have the ability to transition from one combination of speed and load to a second combination of speed and load.

In order to ensure that the variable valve actuator has the ability to make adjustments in combustion phasing both in a retarding and an advancing direction, the variable valve actuators should be controlled with a nominal signal between available retarding and advancing extremes. Because of the relative sluggishness of the geometric compression ratio control device and adjustments to the exhaust gas recirculation rate, engines 10 and 110 of the present disclosure may rely primarily upon the variable valve actuator for a change in the charge mixture, compression ratio and initial cylinder pressure in a sequential engine cycle. On the other hand, electronically controlled fuel injectors have long been able to adjust fuel injection amount from one engine cycle to another. FIG. 6 is also useful for illustrating that the limited band width available for the variable valve actuator about a nominal setting or signal, limits how much the compression ratio can realistically be changed from one engine cycle to another. In addition, dropping compression ratio too quickly can lead to stability problems. Thus, one could expect the HCCI engine 10 and 110 to have the ability to quickly change from a first combination of engine speed and load to a second combination of speed and load that is within the available band width of the variable valve controller plus whatever changes can be made to the geometric compression ratio and exhaust gas circulation rate in single consecutive engine cycle. Although the complete bandwidth of fuel injector quantity control signals may be available on a consecutive engine cycle, only a limited change in charge mixture and compression ratio can be accomplished. In addition, that change is necessarily limited to the speed of the other actuators and there respective bandwidths. For practical purposes, any change in transitioning from a first combination of speed and load to a second combination of speed and load necessarily requires adjusting a variable valve control signal away from the nominal variable valve control signal setting. When the second combination of engine speed and load correspond to a compression ratio and/or charge mixture beyond the ability of the controllers to transition to in a single consecutive engine cycle, a transition will necessarily take a plurality of consecutive engine cycles.

In order to enable the variable valve controller to further adjust compression ratio and charge mixture in a subsequent engine cycle, at least one of the geometric compression ratio control signal and exhaust gas recirculation control signal must be adjusted toward their new target values associated with a transition combination of engine speed and load. These adjustments in geometric compression ratio and exhaust gas recirculation rate, which are relatively sluggish, enable the variable valve actuator to be reset or readjusted back toward the nominal variable valve control signal so that the full bandwidth of the variable valve actuator is again available in a subsequent engine cycle. Assuming that the second combination of engine speed and load are within the control band width of the variable valve actuator, one could expect the engine to transition to the fuel injector control signal and charge mixture and compression ratio associated with the second combination of engine speed and load in a consecutive engine cycle via adjustments to the fuel injector control signal and the variable valve control signal. Thereafter, in the subsequent one or more engine cycles, the more sluggish controllers of the geometric compression ratio control device in the exhaust gas recirculation rate control would move toward and arrive at their new set points as per a map stored in memory as discussed earlier. One could expect the variable valve actuator control signal to be readjusted back toward the nominal variable valve control signal as the geometric compression ratio and exhaust gas recirculation rates approach their target rates.

Not only is the variable valve actuator heavily relied upon to make quick transitions from a first combination of engine speed and load to a second combination of speed and load, but the variable valve actuator also does extra duty in having its control signal adjusted for each of the different engine cylinders to compensate for differences between the actual or sensed combustion phasing. Not only does the variable valve actuator have to do double duty in facilitating the transition while also balancing combustion phasing among the engine cylinders, the fuel injector must also do double duty in facilitating a load change while also balancing combustion heat release among the plurality of engine cylinders. Thus, the engine cylinders will be moving as a group in a direction toward the second combination of engine speed and load, but one could expect the individual control signals associated with the variable valve actuator and the fuel injector for each individual cylinder to be slightly different in order to achieve the combustion balancing among the cylinders. Although not necessary, the engine controller may be set up to determine adjustments in the fuel injector control signal via a first control loop, and determining the variable valve control signal via a second control loop. These first and second loops may be executed at different rates, or the same rates without departing from the scope of the present invention. However, in one embodiment, the second control loop associated with the variable valve actuator is executed at a faster rate than the first control loop associated with the fuel injector control signal. Thus if the electronic controller includes a micro processor with a certain clock speed, different calculations would take place at different frequencies corresponding to this strategy.

Those skilled in the art will appreciate that further mixing control signals may have been predetermined for each engine speed and load across engine operating range in order to arrive at some preferred combination of undesirable emissions. For instance, the end of injection timing will effect how well the fuel and air mix before autoignition conditions arise and the fuel combusts, and hence influence the resulting emissions from that combustion event. In addition, the fuel system may also have the ability to adjust fuel injection pressure, which can also be thought of as a mixing control signal that will influence the emissions resulting from the combustion event. Those skilled in the art will appreciate that laboratory testing will allow one to arrive at the specific geometric compression ratio and exhaust gas recirculation rate settings for a given engine speed and load, and then vary the fuel injection pressure and/or end of injection timing to fine tune the emissions combination at that speed and load. These mixing control signals can then be also stored to further enhance the ability of the HCCI engine to achieve a low desired combination of NOx, unburnt hydrocarbons and particulate matter at each engine speed and load.

INDUSTRIAL APPLICABILITY

Those skilled in the art will recognize that, unlike conventional diesel engines, homogenous charge compression ignition engines may require substantially larger amounts of EGR in order to better facilitate operation across a broad range of speeds and loads of the engine. In fact, these EGR rates may exceed 50% of the gas being supplied to the intake of the engine. These extremely high levels of exhaust gas recirculation are typically not available in exhaust gas recirculation systems associated with conventional diesel engines. Thus, when engines 10 and 110 are operating in the highest portions of there load ranges, increased proportions of exhaust gas are supplied in the recirculation systems 20, 120 by throttling the fresh air intake valves 27 in order to promote the higher EGR levels. In the case of engine 10 at lower speeds and loads, throttle control valve 27 may be positioned in a fully opened condition, whereas the relative proportions of desired EGR are maintained by appropriately positioning control valves 26 and 28 associated with the low and high pressure exhaust gas passages, respectively. On the other hand, the engine of 110 controls the relative proportions of exhaust gas to fresh air by adjusting the position of throttle control valve 27 across the engines operating range.

Those skilled in the art will appreciate that exhaust gas can be useful in manipulating ignition timing, pressure rise rate and the maximum pressure of a combustion event in a homogenous charge compression ignition engine. Because the chemical constituents of the exhaust typically are of higher heat capacity than those of pure air, increasing the percentage of inducted exhaust gas can serve as a heat sink to absorb combustion energy that might otherwise result in an extreme pressure spike. Thus, elevated levels of exhaust gas can reduce peak cylinder pressure and cylinder pressure rise rates, by slowing the combustion rate and retard ignition timing, which will allow for operation at ever higher loads. With all other things being equal, an increased percentage of inducted exhaust in the cylinder will also allow for an increased compression ratio for a given combustion phasing and vice versa. Thus, increased amounts of EGR can be used to retard ignition timing, whereas reduced EGR rates can be utilized to advance ignition timing. Thus, varying amounts of exhaust gas recirculation coupled with a variable compression ratio device and/or the variable intake valve actuator can provide three useful control levers for adjusting ignition timing and maximum cylinder pressure across a wide range of operating conditions.

Those skilled in the art will also appreciate that some attention should be paid to balancing the desire to boost intake pressure by extracting energy from the exhaust gases via turbocharger(s), verses routing exhaust gas for recirculation prior to extracting all of the potential energy therefrom. This issue is addressed in the engines 10 and 110 by including staged turbochargers 122 and 123 in series with one another. However, the present disclosure contemplates a single turbocharger for the engine or possibly two or more turbochargers in series and/or parallel with an appropriate arrangement that allows for sufficient intake boost pressure while allowing for increased exhaust gas recirculation rates associated with homogeneous charge compression ignition operation at higher speeds and loads. Those skilled in the art will appreciate that all of the strategies disclosed above for varying cylinder pressures and cylinder pressure rise rates are closely coupled. Thus, one might wish to rely largely on the variable compression ratio device for bulk changes in compression ratio, rely upon varying amounts of EGR to adjust ignition timing, and may rely upon variable intake valve actuator for quick adjustments from cycle to cycle and to adjust for differences among the cylinders in their behavior. Nevertheless, the control inputs can be mixed and utilized as desired to achieve a desired response time and arrive at a new operating condition with sufficient control capabilities available to operate the engine in any desired fashion.

In order to extend the operating range of engine 10, 110 into higher load ranges, it may be necessary to reduce variations among the engine cylinders 14 in at least one of combustion phase timing and combustion heat release. Those skilled in the art will appreciate that the maximum load capability for an engine occurs when at least one of the engine cylinders produces a peak cylinder pressure or pressure rise rate at or above some predetermined threshold associated with the containment capabilities and/or vibration limits of the engine housing (e.g., engine block and engine head, etc.). By adjusting combustion phase timing, the variation among the individual cylinders 14 can be reduced and the load range extended since all of the cylinders will approach the peak cylinder pressure limit or pressure rise rate limit more in unison rather than one early firing cylinder reaching its limit at a lower load condition. The load range of engine 10, 110 is also extended by adjusting control signals to individual fuel injectors 16 to reduce variations among the engine cylinders with respect to combustion heat release. Thus, if one cylinder has a higher than average combustion heat release, its control signal would be shortened toward a direction of injecting slightly less fuel, whereas a cylinder with a low combustion heat release would have its fuel injector control signal extended to inject slightly more fuel. By power balancing the cylinders, the sound and vibration emissions from the engine can be reduced, especially at higher loads, and the entire engine can be operated at higher loads than that realistically practical or possible with unbalanced cylinders.

In the illustrated embodiment, the maximum load range capability of the engine is maintained throughout its operation by operating the combustion phase timing variation reduction strategy and the combustion energy release variation strategy in a closed loop fashion in the background of the engine operation control. Thus, one could expect the control signals to the fuel injectors 16 and variable intake valve actuators 18, 81 to the individual cylinders 14 to constantly be adjusted to compensate for variations in the combustion phase timing and combustion heat release among the engine cylinders due to inherent factors associated with the engine, and other factors. For instance, inherent variations in the fuel injectors can be compensated for as well as variations resulting from intake manifold geometry. However, by continuously operating the variation reduction algorithm in the background, other sources of variation in combustion phase timing and combustion energy release, such as fresh air pressure, fresh air temperature, engine temperature, EGR temperature and the like can also be compensated for.

Setting up a homogeneous charge compression ignition engine can be accomplished by identifying a combination of compression ratio and exhaust gas percentage that satisfy a pressure rise rate limit and a peak cylinder pressure limit for the engine structure. In order to reduce the number of variables involved, this aspect of the disclosure can be carried out utilizing a single cylinder test engine. However, fully carrying out an identifying process in this regard on a multi cylinder engine may necessarily be accomplished better after the cylinders have been balanced for a combustion heat release and for variations in combustion phase timing. Thus, by utilizing a single cylinder engine for this identification process, some of the complexity in variation can be removed. One might identify a compression ratio and exhaust gas percentage at each speed and load, and then convert the compression ratio and exhaust gas percentages into controller settings for the specific engine. For instance, the compression ratios identified may correspond to geometric compression ratio settings, whereas the exhaust gas percentages would correspond to different settings of the control valves associated with the exhaust gas recirculating system. These settings could then be mapped against speed and load, and the map stored on a medium linked to the electronic engine controller 29. Thus, when the controller determined at what speed and load operation should be maintained, the look up table map would provide settings both for the geometric compression ratio controller system and the exhaust gas controller system. Sensors could allow the controllers to be fine tuned in a closed loop fashion to precisely represent these desired values, or they may be set in an open loop manner. Because of the subtleties of operation, it may be desirable to have closed loop control over the exhaust gas return rate settings, whereas open loop control may better suffice with regard to geometric compression ratio controller. When employing these settings then in a multi cylinder engine, the electronic engine controller should be configured to balance combustion phasing, and possibly combustion heat release among the plurality of engine cylinders so that any imbalance is reduced. In other words, without balanced cylinders, an uncorrected imbalance alone can limit high load operation even if appropriate settings are otherwise available. As stated earlier, this is because one cylinder will arrive at peak cylinder pressure limit or peak cylinder pressure rise rate limits prior to the rest.

Generally, these settings may be arrived at by first finding an exhaust gas percentage that achieves a desired NOx level output from the engine while also satisfying a peak rise rate limit and avoiding either a smoke or misfire limit as shown in FIG. 5. Next, a compression ratio is identified at that exhaust gas percentage that results in a desired combustion phasing. Mixing controls, namely end of injection timing and injection pressure may also be determined at this time. Those skilled in the art will appreciate that reducing geometric compression ratio retards ignition timing, and increasing geometric compression ratio generally advances combustion phasing. Because virtually all settings have an interrelated effect, the desired settings may be arrived at in an iterative manner. Thus, one may wish to go back and readjust the exhaust gas return rate setting to readjust the NOx level to a desired state. Next, the geometric compression ratio can again be adjusted to fine tune combustion phasing, given the exhaust gas return rate setting. The mixing controls may also be part of the iterative process. This iterative process may continue at each speed and load until the engine operates in a desired fashion and produces a mixture of acceptable levels of emissions, including NOx, unburnt hydrocarbons and particulate matter. Nevertheless, those skilled in the art will appreciate that the higher load ranges almost necessarily require that the combustion balancing previously discussed to be put in effect. Those skilled in the art will appreciate that identifying compression ratio and exhaust gas return rate settings using this methodology can be quite cumbersome when finding an appropriate recipe at each speed and load across an engines operating range. However, these predetermined settings allow the controller to always know where it should be, and leave the finer quick control aspects of the engine to the variable valve actuators and fuel injectors that would require individual control signals for each one of the cylinders.

When operating in steady state conditions, and assuming that no balancing in either combustion phasing or heat release is required among a plurality of cylinders, one could expect the geometric compression ratio control signal, the exhaust gas return rate control signal and the mixing control signals to be at their map values. In addition, one could expect the variable valve control signal to be at its nominal value, and the combustion phasing and heat release to be at their desired values. When one folds into this concept the realization that heat release and combustion phasing will inherently vary due to factors discussed above in each of the engine cylinders. The individual control signals for the variable valve actuator and fuel injectors will be slightly different for each cylinder, however, the control signals will be close, and one could expect the variable valve control signals to all be in the vicinity of the nominal variable valve actuator control signals so that it has the ability to change combustion phasing in either a retarding or advancing direction within the available band width. Each cylinder can be thought of as having an individually different nominal signal.

Although the strategy for transitioning from a first combination of engine speed and load to a second combination of speed and load was discussed above, the engine controller may also have specific maps available for transitioning between different combinations of engine speed and load. For instance, there might be different transition strategies mapped for different magnitudes of acceleration and deceleration. In addition, these strategies may be different when accelerating in different areas of the engine operating range. For instance, although the general concepts above may be applicable when accelerating or increasing load in any point in the engine operating range, one might expect a slightly different sequence of control signals when changing from idle than when maybe changing from a medium speed and load to a high speed and load. Thus, in either case, one could expect the variable valve actuator to facilitate a quick change in charge mixture and compression ratio by being adjusted away from its nominal control signal setting in a consecutive engine cycle. Thereafter, in at least one subsequent engine cycle(s), the more sluggish exhaust gas recirculation rate controller and geometric compression ratio controller would move toward their new map set points associated with the second combination of engine speed and load so that the variable valve actuator can be readjusted toward its nominal setting, and reenable its full bandwidth of control for tuning combustion phasing and being prepared for the next change in engine speed and load.

Those skilled in the art will appreciate that much of the above discussion assumes that different actuators can react at different rates. In general, the exhaust recirculation rate can not change nearly instantaneously from one engine cycle to another and almost will inherently be the most sluggish control lever available to the controller. However, this disclosure does contemplate other HCCI engines where geometric compression ratio might be quickly changed, and may have an individual control actuator associated with each of the individual cylinders. In such a case, those skilled in the art will appreciate that the concepts above would be equally applicable, but the quick change from one combination of engine speed load to a second combination of speed load will necessarily fall upon those actuators that can most quickly change from one engine cycle to the next. In the illustrated embodiment, it is the fuel injector and variable valve actuator that can adjust from one engine cycle to the next, but the variable valve actuator only has a limited bandwidth. In other HCCI systems, a different combination of controllers might be relied upon for quick changes, and slower actuators might be utilized to reset the combustion phasing control actuator for subsequent changes and tuning combustion phasing among a plurality of engine cylinders.

It should be understood that the above description is intended for illustrative purposes only, and is not intended to limit the scope of the present invention in any way. Thus, those skilled in the art will appreciate that other aspects of the invention can be obtained from a study of the drawings, the disclosure and the appended claims. 

1. A method of operating an engine, comprising the steps of: compressing a charge mixture of air, exhaust and fuel in a combustion chamber to an autoignition condition of the fuel; transitioning from a first combination of speed and load to a second combination of speed and load by changing the charge mixture and compression ratio; the changing step includes adjusting, for a consecutive engine cycle, both a fuel injector control signal and a variable valve control signal away from a nominal variable valve control signal; and the changing step includes re-adjusting the variable valve control signal back toward the nominal variable valve control signal by adjusting at least one of a geometric compression ratio control signal and an exhaust gas recirculation control signal over at least one engine cycle following the consecutive engine cycle.
 2. The method of claim 1 including a step of sensing a combustion phasing; determining a desired combustion phasing; and adjusting the variable valve control signal based upon a difference between the sensed combustion phasing and the desired combustion phasing.
 3. The method of claim 1 wherein the transitioning step includes determining a desired combination of exhaust gas recirculation and geometric compression ratio based upon the second combination of speed and load.
 4. The method of claim 3 including a step storing a desired combination of exhaust gas recirculation and geometric compression ratio for different combinations of engine speed and load across an operating range of the engine.
 5. The method of claim 1 including a step of balancing combustion events among the different combustion chambers.
 6. The method of claim 5 wherein the balancing step includes balancing combustion phasing and heat release by determining individually different control signals to variable valve controllers and fuel injectors of different combustion chambers.
 7. The method of claim 6 including a step of determining a timing and magnitude of a peak pressure rise rate for combustion events in the different combustion chambers; and the balancing step includes trimming variable valve control signals and fuel injector control signals to the different combustion chambers responsive to the determined timing and magnitudes of the peak pressure rise rates, respectively.
 8. The method of claim 1 including a step of storing fuel and air mixing control signals for different combinations of engine speed and load across an operating range of the engine.
 9. The method of claim 8 wherein the fuel and air mixing control signals includes an end of injection timing aspect of the fuel injector control signal and a fuel injection pressure control signal.
 10. The method of claim 1 wherein the adjusting step the fuel injector control signal via a first control loop, and determining the variable valve control signal via a second control loop; and executing the second control loop at a faster rate than the first control loop.
 11. An engine comprising: means for compressing a charge mixture of air, exhaust and fuel in a combustion chamber to an autoignition condition of the fuel; a fuel injector responsive to a fuel injector control signal; a variable valve actuator responsive to a variable valve control signal; at least one of a geometric compression ratio device responsive to geometric compression ratio control signal and an exhaust gas recirculation control valve responsive to an exhaust gas recirculation control signal; means for transitioning from a first combination of speed and load to a second combination of speed and load; the means for transitioning including a means for adjusting the fuel injector control signal and the variable valve control signal away from a nominal variable valve control signal in a consecutive engine cycle; the means for transitioning also including a means for adjusting at least one of the geometric compression ration control signal and the exhaust gas recirculation control signal over at least one engine cycle following the consecutive engine cycle; and the means for transitioning further including a means for re-adjusting the variable valve control signal back toward the nominal variable valve control signal.
 12. The engine of claim 11 including: an engine housing having at least one combustion chamber; a fuel injector positioned for direct injection of fuel into each of the at least one combustion chamber; at least one gas exchange valve for each of the at least one combustion chamber; a variable valve actuator operable coupled to a gas exchange valve of each of the at least one combustion chamber; an exhaust gas recirculation control valve; a variable geometric compression ratio device for varying a geometric compression ratio of the at least one combustion chamber; the means for transitioning including an electronic controller in control communication with the fuel injector, the variable valve actuator, the exhaust gas recirculation control valve and the variable geometric compression ratio device.
 13. The engine of claim 12 wherein the controller is configured to determine desired exhaust gas recirculation and geometric compression ratio based upon the second combination of speed and load.
 14. The engine of claim 13 including at least one exhaust recirculation sensor in communication with the electronic controller the electronic controller is configured to determine the control signal for the exhaust gas recirculation control valve based upon the desired exhaust gas recirculation and the sensed exhaust recirculation.
 15. The engine of claim 14 including at least one combustion sensor; and the electronic controller is configured to determine different control signals for each variable valve actuator of the plurality of combustion chambers based upon the sensed combustion.
 16. The engine of claim 15 wherein the electronic controller is configured to determine combustion phasing and combustion heat release for each of the combustion chambers; the electronic controller is configured to determine different fuel injector control signals among the combustion chambers based on the determined heat release among the combustion chambers; and the different control signals for each variable valve actuator being based on the determined combustion phasing for each of the combustion chambers.
 17. The engine of claim 16 including a storage medium with mappings of desired combinations of exhaust gas recirculation and geometric compression ratio for different combinations of engine speed and load across an operating range of the engine.
 18. The engine of claim 17 wherein the at least combustion sensor includes a pressure sensor for each of the combustion chambers and the electronic controller is configured to determine timing and magnitudes of peak pressure rise rate for each of the combustion chambers; and the determined combustion phasing and heat release are based on the determined peak pressure rise rate timing and magnitude for respective combustion chambers.
 19. The engine of claim 18 wherein the storage medium includes mappings of fuel and air mixing control signals for different combinations of engine speed and load across an operating range of the engine.
 20. The engine of claim 19 wherein the fuel and air mixing control signals include end of injection timing aspect of a fuel injector control signal and a fuel injection pressure control signal.
 21. The engine of claim 20 including a geometric compression ratio sensor in communication with the electronic controller; and the electronic controller is configured to determine the variable geometric compression ratio control signal based on the desired geometric compression ratio and the sensed geometric compression ratio. 